OGIP Calibration Memo CAL/ROS/92-001
The On-Axis Point Spread Function:
In-flight comparison with the PANTER results
Günther Hasinger,
& Günter Boese
Code 668,
Version: 1995 May 11
NASA/GSFC,
Greenbelt, MD20771
The components of the ROSAT PSPC on-axis point spread function (psf) are discussed, and a direct comparison made between the predicted psf from ground calibration measurements and in-flight data obtained during the early part of the mission. It is found that the analytical functions derived from the ground calibration data satisfactorily describe the 5 in-flight datasets tested here.
Release | Sections Changed | Brief Notes |
Date | ||
1992 Oct 05 | Published in Legacy, 2, 77 | |
1995 Jan 19 | All | Made compatible with LaTeX2HTML software |
1995 Feb 07 | All | Attempt to fix LaTeX2HTML problems |
1995 May 09 | 4 | Several Figures added |
The psf of the ROSAT X-ray mirror assembly
(XMA) + PSPC is a convolution of several component:
These are individually discussed in more detail below.
Specifically the on-axis psf is described in detail,
comparing the form derived from an analysis of ground calibration
data with that obtained in orbit.
The off-axis psf will be discussed in more detail in
a future OGIP calibration memo.
Throughout,
Microroughness of the reflecting mirror surfaces leads to non-specular
reflection of X-rays, ie scattering.
Theoretically, assuming the grazing angle remains constant,
the scattering fraction should increase as E2.
Due to the laws of diffraction, the shape parameters should
be µ E-1.
The importance of scattering by the ROSAT XMA is small compared to
previously available X-ray mirrors, offering the ability to perform
high contrast imaging. The form of the scattering is a complex function of
energy, grazing angle and the scale size of the mirror surface roughness.
The combination of these effects can be modelled as a Lorentzian which
breaks to a power law at high radii.
The off-axis psf of grazing incidence optics is rather complicated.
A convenient measure of the image spread is the so-called RMS blur radius,
defined as the radius within which 68% of the photons fall, ie the Gaussian
sigma of the distribution of photons for a given off-axis angle.
The expected ROSAT XMA rms blur circle radius, rblur,
increases rapidly with off axis angle.
The off-axis effects will be treated in a
subsequent psf memo.
Due to the inherent statistics of the primary electron generation,
the intrinsic spatial resolution of the ROSAT PSPC is
expected to be a gaussian.
Theoretically its width is µ E-1/2 and
independent of q.
The design distance between the XMA and
PSPC (the window of which is flat) is such that
photons of ~ 1 keV on-axis source are brought to a focus
(along a surface of a cone of half-angle 8.5ƒ) at
an optimum depth within the PSPC drift region
such that the gaussian spatial distribution of pulses on the cathode
wires is minimized.
Consequently the image of a point source is sharpest at 1 keV.
The position of an event in the PSPC is determined from the amplitudes
of signals on the two cathode grids. The specific algorithm uses the
two highest signals from each cathode grid (the cathode grids are divided
into something like 22 segments with separate amplifiers). For events
with large pulse-height amplitudes, this works very well since the
strength of the signals on the cathode segments is related to the
strength of the signal on the anode. However, for small pulse-height
amplitudes, occasionally only one cathode segment of a grid will have a
signal above the lower discriminator. This still gives a well specified,
but incorrect, position.
If two segments of one
grid have signals but only one of the segments from the other grid has a
signal, then the determined position will lie along a line. If only one
segment from each grid has a signal, then the determined position will lie
at a point. This structure is very apparent when looking at an image of
events in detector coordinates with pulse heights less than channel
15 ( ~ 0.15 keV).
There is a cross-work pattern of lines with bright spots at the
intersections. There are secondary bright spots in the centers between
the lines since the probability is greater there to get signals on four
cathodes.
Generally, SASS processing allows only data of good attitude solution
to be included in the "Good-Time Intervals" (GTIs).
Only data with attitude solutions better than ~ 2 arcsec are included
in the GTIs for sequences processed by SASS
after 1991 Dec (earlier processing had a looser constraint on the
attitude solution, sometimes resulting in a noticeable asymmetric blurring
of the image).
The detailed psf parameters and their associated E dependences have been
determined for PSPC-A & PSPC-C using 4 monochromatic energies
(0.28, 0.93, 1.49 & 1.70 keV) at the PANTER test facility in Garching.
Currently, results for three of the components of the psf have been
determined - namely the PSPC intrinsic resolution, focus and penetration
effects and the effects due to mirror scattering.
In principle the resultant three components should be folded with each
other, however, they are sufficiently well separated in the r (spatial)
domain that MPE considers a simple addition accurate enough.
The analytical form derived for the fraction of photons within this
component as a function of energy is given by:
1 INTRODUCTION
q is the off-axis angle (in arcmin) from the centre of
the PSPC field of view,
r is the radius (in arcmin) from the PSF centroid,
PSF(E,r) is the psf (in normalized cts area-1),
and
E is the photon energy (in keV).
1.1 The XMA Scattering Profile
1.2 The Off-axis Blur of the XMA
1.3 The Instrinsic Resolution of the Counter
1.4 Focus and Penetration Effects
1.5 Ghost Images
1.6 Ellipsoidal blur due to residual attitude motion
2 GROUND CALIBRATION DATA
2.1 The XMA Scattering Profile
| (1) |
The PANTER tests confirmed that this component was well approximated by a lorentzian, as expected (Section 1.1), steepening to a powerlaw at large r, ie
|
| (3) |
| (4) |
The width of the lorentzian, rscatt, as a function of energy was found to be:
| (5) |
The normalization of the lorentzian, Ascatt,is given by
| (6) |
| (7) |
| (8) |
The fraction of incident photons scattered outside a radius, rcell, is shown as a function of energy for various rcell in Figure 5. It should noted that at 1 keV, ~ 6% of incident photons will be scattered outside rcell = 100 arcsec, and ~ 5% outside rcell = 10 arcmin.
To summarize:
At low energies, the strength of this component to the psf is
very small, and its width very large, making it
difficult to distinguish this component from the background and/or
slow variations in the efficiency of the PSPC.
As one moves to higher energies (above ~ 0.5 keV),
the strength of the component increases
and the width decreases, increasing the importance of this component
to the total psf (see Figures 6a &
6b).
At energies for which the analytical parameterization of the PANTER data is valid (ie less than ~ 2 keV), the steepening from a lorentzian to a powerlaw form occurs at radii, rb greater than ~ 10 arcmin. Since the break is relatively gentle (Da less than ~ 0.4), this is unlikely to be detectable in most datasets.
All photons not in the other 2 components are assumed to be in this component. Thus the fraction of photons within this component as a function of energy is given by:
| (9) |
The PANTER tests confirmed that this component was well approximated by a gaussian, as expected from the statistics of the primary electron generation process (Section 1.3); ie
| (10) |
| (11) |
The normalization, Aint(E), is given by
| (12) |
The analytical form derived for the fraction of photons within this component as a function of energy is given by:
| (13) |
The combined contribution of focussing and the finite penetration of photons into the counter on the psf can be is modelled as an exponential function:
| (14) |
The e-folding angle, rt, was found to be given by
| (15) |
The normalization, Aexp(E), is given by
| (16) |
To summarize:
The fraction of the photons
within this component increases with E (Figure 1);
the normalization of the resultant exponential component to the psf
increases with E, then flattens off at ~ 1 keV; whilst
the e-folding angle (rt) decreases with E for energies below
~ 1 keV, then increases with E at higher energies.
The predicted composite psf, PSFtot, for the ROSAT XMA + PSPC combination at a given energy is given by the addition of the components given above (ie PSFscatt + PSFint + PSFexp). Examples of PSFtot are shown in in Figures 6a & 6b (solid lines) at several energies, along with curves showing the three individual components. In Figure 7 are shown the corresponding curves of the predicted encircled fraction as a function of radius. For convenience, the radii encircling 50, 90, 95 & 98% of the photons are also listed in Table 2.4 and plotted in Figure 8. It can be seen that above ~ 1 keV, it is predicted that a substantial fraction ( ~ 5%) of photons will be scattered by the XMA outside a radius r ~ 10 arcmin (see also Figure 5).
Energy | Radius (arcmin) | |||
(keV) | 50% | 90% | 95% | 98% |
0.188 | 0.44 | 0.81 | 0.94 | 1.14 |
0.284 | 0.36 | 0.68 | 0.79 | 0.99 |
0.5 | 0.29 | 0.54 | 0.65 | 2.20 |
1.0 | 0.22 | 0.45 | 1.55 | > 10 |
1.7 | 0.28 | 1.36 | 8.79 | > 10 |
In Figure 9, the predicted psf is compared directly with the PANTER data from which it was derived. It can be seen from the residuals that the fits are generally satisfactory, particularly at radii greater than ~ 1 arcmin.
It should be emphasized that the above analytical parameterizations are only valid over the energy range 0.15 < E < 2.0 keV (ie channels 15-200).
The above Ground Calibration results have been tested against the in-flight datasets listed in Table 3.1. The letter in parentheses after the ROR number indicates which PSPC was used to obtain the data (PSPC-C was in use prior to its destruction during the sun pointing on 1990 Jan 25). Whilst ideally we would have preferred to use bright calibration sources, many of the sources observed in the first calibration phase are unsuitable for this study. AR LAC was never observed on-axis with the PSPC (in the first calibration datasets) and many of the other calibration targets are extended, often due to the presence of a dust halo. Some satellite maintenance observations which have been made more recently will be used to check these results, but in the meantime we have tested against several point source datasets. Two of the datasets were from the long pointing phase and hence provide excellent signal-to-noise. In any cases where there was some evidence for an extended feature in the point source, or where there were other sources close to the on-axis point source, suitable exclusion regions were set for the profile extraction. Data attitude solutions were checked, and any data with attitude error greater than 2 arcseconds was excluded from the analysis.
No. | ROR | Object | Class | Exp (ksec) | Comment |
1 | rp150071 (C) | NGC5548 | Seyfert 1 | 18.86 | PV |
2 | rp700055 (B) | NGC3998 | LINER | 22.85 | AO1 |
3 | rp700057 (B) | Pictor A | LINER | 4.46 | AO1 |
4 | rp700105 (B) | Mkn509 | Seyfert 1 | 1.77 | AO1 |
5 | rp700104 (B) | ESO141 | Seyfert 1 | 5.02 | AO1 |
Radial profiles were extracted using PROS in the five energy bands listed in Table 3.1. Five was considered optimum for energy resolution with good signal to noise in each band. Typically several thousand counts per source per bandpass were obtained for comparison with the predicted psf.
Name | Energy (keV) | PI Channels | ||
min | max | min | max | |
B | 0.10 | 0.188 | 9 | 18 |
C | 0.188 | 0.284 | 19 | 29 |
R1 | 0.284 | 0.5 | 30 | 50 |
R2 | 0.5 | 1.0 | 51 | 101 |
R3 | 1.0 | 2.48 | 102 | 256 |
The lowest 8 channels were rejected to exclude problems due to the variable lower limit discriminator for valid events, due to the variable instrument gain which is folded into these data.
The following specifications were applied to the data:
Any additional sources falling within the specified annuli were masked out of the analysis as noted above.
No background subtraction was carried out. Background rates were measured from the images and were later folded into the predicted profile template for each source in each band. The background count rates are detailed in Table 3.1, and are generally in good agreement with those expected.
The counts profiles extracted were normalized to counts per square arcminute and the data dumped to ascii files, suitable for fitting in QDP.
The counts profiles were rebinned such that each spatial bin contained at least 20 photons.
No. | ROR | Bkgd | c2/Np |
(ct arcmin2) | |||
B-band | |||
1 | rp150071 (C) | 1.4×10-3 | 282/27 |
2 | rp700055 (B) | 8.6×10-3 | 832/39 |
3 | rp700057 (B) | 7.2×10-3 | 192/9 |
4 | rp700105 (B) | 1.5×10-3 | 41/14 |
5 | rp700104 (B) | 3.3×10-3 | 57/14 |
C-band | |||
1 | rp150071 (C) | 9.2×10-4 | 68/22 |
2 | rp700055 (B) | 5.1×10-3 | 295/36 |
3 | rp700057 (B) | 4.0×10-3 | 62/13 |
4 | rp700105 (B) | 8.6×10-4 | 65/15 |
5 | rp700104 (B) | 1.5×10-3 | 29/17 |
R1-band | |||
1 | rp150071 (C) | 7.6×10-4 | 56/19 |
2 | rp700055 (B) | 3.5×10-3 | 143/26 |
3 | rp700057 (B) | 4.0×10-3 | 27/12 |
4 | rp700105 (B) | 7.5×10-4 | 18/12 |
5 | rp700104 (B) | 1.2×10-3 | 53/16 |
R2-band | |||
1 | rp150071 (C) | 5.5×10-4 | 15/17 |
2 | rp700055 (B) | 1.0×10-3 | 66/24 |
3 | rp700057 (B) | 1.8×10-3 | 47/16 |
4 | rp700105 (B) | 2.5×10-4 | 17/12 |
5 | rp700104 (B) | 6.8×10-4 | 39/20 |
R3-band | |||
1 | rp150071 (C) | 5.3×10-4 | 56/22 |
2 | rp700055 (B) | 6.3×10-4 | 31/22 |
3 | rp700057 (B) | 9.4×10-4 | 34/15 |
4 | rp700105 (B) | 1.9×10-4 | 24/14 |
5 | rp700104 (B) | 4.0×10-4 | 37/19 |
The detailed psf parameters and their energy dependence have been determined using the PANTER telescope calibration data of both PSPC-A and PSPC-C at the monochromatic energies 0.28, 0.93, 1.49 and 1.70 keV. At lower pulseheights than channel 15 (0.15 keV) additional 'ghost images' appear in the PSPC, as described in the previous section, for which no analytical fit is possible. Fits to the B band data are shown to illustrate this point. We will return to this point in the summary.
As the in-flight data are affected by more uncertainties than the ground data (aspect corrections, background subtraction, gain correction etc) it was not possible to allow profile fitting with the parameters of the gaussian + exponential + lorentzian components to be free. Instead we calculated the psf for every source in each bandpass.
First, a spectrum was extracted for each source, in a circle of size several arcminutes radius (exact region mask used depended on the particular field) to ensure that essentially all of the sources counts were collected. Next, a psf was calculated for each energy channel. A predicted psf template was calculated for each dataset using the source spectrum to determine the photon weighting to be applied to the psf component in each energy channel. Thus for each band and spectrum a combined psf was produced, including a constant term for the background component from Table 3.1.
These predicted templates were overlaid on the appropriate datasets as illustrated in Figures 10a, 10b, 10c, 10d, 10e. As the normalization of the model was also calculated (using the equations in Sections 2.1, 2.2 and 2.3), NO FITTING was performed. The c2-statistic for each dataset and band is listed in Table 3.1. It can be seen that, except in the case of the B band, the model generally gives a good description of the psf. Some slight discrepancies are observed, as can be seen from Figures 10a, 10b, 10c, 10d, 10e (particularly the case for NGC 3998). As NGC 3998 is a nearby galaxy, part (or all) the deviation observed in this source may be an indication of genuine extended X-ray emission. This and the fact that no systematic deviations are observed across the other datasets tested leads us to conclude that the psf model should not be modified based on the NGC 3998 deviations alone. Comparison of more point source datasets should be made before we can determine whether effects such as this should be modelled.
The MPE model for the PSPC psf is good for energies between 0.15 and 2.0 keV. Generally the predicted shape agrees well with the data, with no obvious systematics in any band except the B-band. Thus, within the statistical limits of these datasets, we conclude the model is a satisfactory description of the PSPC psf. More bright source datasets are expected to become available to the ROSAT GOF within the next few months. These may provide a more stringent test of the model, and any discrepancies found will be noted in future OGIP Calibration Memos.
The MPE model does not satisfactorily predict the observed B-band psf. Whilst Figure 10a illustrates the effect of Ghost imaging at low energies, this effect is not (yet) quantifiable. Thus at present, it is recommended that users extract data products within a large enough region such that most the B-band counts are included and a negligible correction is required (see Figure 7 and 8).
We thank the many people at MPE involved in the determination & interpretation of the PANTER data, Dave Davis (GSFC) for his help extracting the data and Gail Reichert (GSFC) for supplying some test datasets from her own AO-1 observations.
The following useful links are available (in the HTML version of this document only):
1 Note that due to a typographical error there was a factor 2 missing from the following equation in all versions of this memo prior to 1992 Oct 05 (the software used to generate the figures was however correct)